Mask defect analysis system

ABSTRACT

An automated system for analyzing mask defects in a semiconductor manufacturing process is presented. This system combines results from an inspection tool and design layout data from a design data repository corresponding to each mask layer being inspected with a computer program and a predetermined rule set to determine when a defect on a given mask layer has occurred. Mask inspection results include the presence, location and type (clear or opaque) of defects. Ultimately, a determination is made as to whether to scrap, repair or accept a given mask based on whether the defect would be likely to cause product failure. Application of the defect inspection data to the design layout data for each mask layer being inspected prevents otherwise acceptable wafer masks from being scrapped when the identified defects are not in critical areas of the mask.

CROSS REFERENCE TO RELATED APPLICATIONS

This application is a divisional application of copending U.S. application Ser. No. 09/683,836, filed on Feb. 21, 2002, the contents of which are expressly incorporated by reference in their entirety herein.

BACKGROUND OF THE INVENTION

1. Field of the Invention

The present invention generally relates to the field of semiconductor manufacturing, and, more particularly, to a method for automating the evaluation and analysis of defects in masks used in the semiconductor manufacturing process to determine which defects would cause product failure.

2. Background Description

As technology in the computer manufacturing field matures, the physical size of semiconductor chips continues to decrease dramatically. Accordingly, increasingly precise techniques and tools are required to manufacture the chips and the circuitry that is to be packaged on the chips. These techniques include the use of masks to create the circuit pattern corresponding to the chip design. It is a common practice in the industry to use masks in the manufacturing process for semiconductor chips. The design and layout of the circuit for the chip can be stored in the form of a mask, which can then be transferred to the surface of a silicon wafer. This process is referred to as photolithography. As the chips become smaller and smaller, the precision required in the masks increases. Therefore, the process for evaluation and inspection of the masks becomes increasingly important to the efficiency of the manufacturing operation.

Accepted techniques for inspection of masks use optical inspection tools to determine the presence of defects on the mask. The output of these tools can then be used in conjunction with pre-established criteria to determine if the defects require the masks to be scrapped, repaired or accepted. The most commonly used criterion is based on the size of the defect; however, defects can also be classified as to location and type (clear or opaque). In any event, the standard inspection process will tend to result in the rejection of masks when the size of the defect exceeds some maximum pre-established criterion. This approach is non-discriminating, however, because it is well known that not all defects in a given mask will necessarily lead to failure of the chip. For example, shorts between dummy fill shapes are generally harmless unless they merge to create a single shape larger than several microns. Also, via to via shorts between vias on the same net are harmless if they do not also cause the vias to expand outward beyond the underlying and overlying metal shapes. Accordingly, the standard approach can lead to the rejection of masks with defects in non-critical regions of the chip layout.

Based on this standard approach, otherwise acceptable masks would be scrapped unnecessarily. Alternatively, such masks must be analyzed manually by a human operator or a defect classification tool. Manual classification of defects, via an optical device or scanning electron microscope, can resolve issues such as whether a particular defect falls on or near dummy fill shapes rather than active circuit elements. However, in general, such techniques cannot resolve issues involving nets because simple inspection of the mask or the layout data does not suffice to accurately define the nets. In any event, either option is labor intensive and expensive and can be detrimental to the manufacturing process.

To improve the manufacturing process it is desirable to have an automated system for analyzing and evaluating the results from the inspection of the masks. An automated system would eliminate unnecessary scrapping of otherwise acceptable masks and would reduce the possibility of human error. Such a system will enhance both the pre-shipment inspection and repair process as well as the pre-acceptance inspection process. By identifying only those mask defects that will lead to chip failure, thereby ignoring the remainder of defects, the efficiency of the inspection/repair and acceptance process will be improved. Moreover, an automated system will allow manufacturers to concentrate on systemic errors that lead to defects in the masks, thereby improving the overall manufacturing process.

SUMMARY OF THE INVENTION

The present invention is directed to a system for analyzing mask defects in a semiconductor manufacturing process, and, more particularly, to a method for automating the evaluation and analysis of defects in the masks to determine which defects would cause product failure.

In one aspect of the present invention, masks used in the manufacturing of semiconductor wafers undergo a standard inspection process designed to locate the presence of defects on the mask. Any one of several commercially available mask inspection tools can be used, such as an optical device. Defect inspection data from that inspection process, which include the coordinates, sizes and types (clear or opaque) of defects, are recorded into a computer. Design data corresponding to an ideal mask (i.e., without defects) are stored in a design data repository, which is accessed for each layer of mask being inspected. In a preferred embodiment, the design data repository is a computer database program and suitable hard disk or other storage sufficient to store multiple large (i.e., over 1 GB) computer files that contain the design layout data. This design layout data is addressable not only by design level, with multiple design levels combining to make up a given layer of the mask, but also by chip part number or other suitable identifier. That design data is modified according to the defect inspection data, and the modified design data is analyzed with a computer program in conjunction with a rule set to determine if a given mask defect is likely to cause product failure. For each mask layer being analyzed, the computer program reads the output from the inspection report and then identifies defects as being present on the mask according to any shapes that do not exist in the design layout data. The computer program then generates shapes corresponding to these defects. A rule set exists for each mask layer being analyzed. The rule set includes criteria for analyzing both intra- and inter-level wafer problems associated with the location, size and type (clear or opaque) of mask defects. Finally, an industry standard design rule checking program is used to apply the rule set to determine whether to scrap, repair or accept the mask based on the current defect. When all defects have been analyzed or a scrap threshold has been reached, a decision is made as to whether any of the defects are likely to cause product failure.

In another aspect of the present invention, the inspection defect data comprises intensity contour plots from a commercially available inspection tool, such as AIMS. The intensity contour plots (also known as aerial images) contain the size, location and type of defect information similar to that provided by an optical inspection tool. In addition, the intensity contour plots provide information on how or if the defect will be resolved on the wafer when the mask image is transferred to the wafer. In this aspect of the present invention, the method for modifying the design data from the design data repository includes creating a simulated wafer image of the defect and merging the simulated wafer image into a simulated wafer image of a semiconductor chip. Thereafter, using the same analysis as that described for the first aspect of the present invention, the rule set is applied to analyze the simulated wafer image except that the rule set is modified to account for the mask magnification factor. This modification is used to scale the defect size and coordinates when the representative defect shape is generated in the layout data such that the rule set is written to be independent of the magnification factor.

In another aspect of the present invention, the method can be applied to both the inspection and the pre-acceptance process. During either process, masks that have defects can be accepted, rather than repaired, if the defects are within acceptable deviations from the design tolerances. This allows the repair process to be skipped altogether if it is determined that the defects so identified will not cause product failure (e.g., defects in non-critical areas of the mask, or defects are within acceptable tolerances). By eliminating unnecessary repairs, the cost and time of repair are saved. Furthermore, this can prevent the defects that are sometimes generated (or exacerbated) by the repair process itself.

In another aspect of the present invention, the system uses a set of heuristic rules for determining whether a given mask defect will be resolved on the wafer by the photolithographic process. Alternatively, that determination can be made using one of a variety of commercially available tools such as NumeriTech's Virtual Stepper™ or the output of the AIMS tool. Heuristic rules for whether or not a defect would be resolved on the wafer would include defect size limits and limits on the defect placement relative to shapes from the design layout data. These rules are developed by empirical data on printed defects as well as photolithographically modeled results. Output from commercially available software (NumeriTech's Virtual Stepper™ or the aerial image data from the AIMS tool) provides a more reliable method of determining whether or not a defect would be resolved on the wafer by modeling the photolithographic pattern transfer process. Ultimately, those mask defects which are resolved on the wafer would then be analyzed to determine if they were problematic.

In another aspect of the present invention, a mask is inspected for defects in order to evaluate the effect of defects. Defect locations are analyzed to classify the defects into critical defects and non-critical defects. The final disposition of the mask is determined by applying different acceptance rules to the critical defects and the non-critical defects. A standard acceptance rule is applied to the defects located in the critical portions of the mask while a loose acceptance rule is applied to the defects located outside of the critical portions. When the loose acceptance rule is applied, the non-critical defects are considered as the candidates for a looser mask acceptance criteria. The critical dimension measurement is selectively performed only to the critical defects and routed to a repair step 240 or a scrapping step 250. Thus, according to the present invention, the time consuming critical dimension measurements are performed restrictedly to the critical portions, thereby speeding up the measurement process.

BRIEF DESCRIPTION OF THE DRAWINGS

The foregoing and other objects, aspects and advantages will be better understood from the following detailed description of a preferred embodiment of the invention with reference to the drawings, in which:

FIG. 1 depicts a mask used in the photolithography process of forming semiconductor wafers;

FIG. 2 contains a block diagram for a mask defect analysis system applied to both an inspection and a pre-acceptance process;

FIG. 3 a depicts design layout data retrieved from a data repository for each mask layer being inspected;

FIG. 3 b depicts shapes generated by a computer program corresponding to defects in the design layout data; and

FIG. 4 is a flow chart of a computer program for analyzing defect inspection data.

FIG. 5 is a process flow chart for determining a final disposition of a component by applying different acceptance rules depending on defect criticality.

DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS

The present invention is directed to a system for analyzing defects in masks used in a semiconductor manufacturing process, and, more particularly, to a method for automating the evaluation and analysis of defects in the masks so as to determine if a given mask should be scrapped, repaired or accepted. The method utilizes defects identified through an industry-accepted inspection process and a design data repository that stores design layout data for each mask being inspected, combined with a predetermined rule set, to identify defects in the masks that would be likely to cause chip failures. By using the method of the present invention, an automated process is provided to determine whether mask defects identified during the inspection process will likely lead to failure of the product.

This method is not directed to determining whether a failure on the mask has occurred. Rather, the present invention relies on the pre-existing mask inspection process, as well as the pre-determined defect criteria, to determine if a defect (but not necessarily a failure) has occurred. Information regarding the defects includes the presence, location and type (clear or opaque) of defects that may have occurred. In turn, the method of the present invention uses that information from the inspection report to identify those masks that will likely cause chip failure and which, if they cannot be repaired, should be scrapped.

Referring now to the drawings, the system of the present invention will be described. FIG. 1 depicts schematically a mask 5 that is used in a semiconductor manufacturing process. The mask includes a clear (i.e., non-opaque) quartz substrate material 7, upon which resides an opaque chromium material 9 laid out in the circuit pattern designed for the semiconductor chip (not shown). The mask manufacturing process is known to be imperfect and can result in defects in the masks. For example, excess chromium material deposits 9 on the quartz substrate 7 (i.e., additional metal deposits in between the layout of the circuit pattern) can ultimately cause shorts in the semiconductor chip. As such, the mask 5 undergoes an inspection process to identify those defects. Unfortunately, the interpretation and use of the results from the inspection process using conventional techniques are labor intensive. Moreover, some defects on the mask are not critical and will not necessitate repairing or scrapping the mask. Therefore, a discriminatory inspection and evaluation system is required. The present invention provides a capability to use results from that inspection process to automate the decision making for determining whether a given mask should be scrapped, repaired or accepted.

In a preferred embodiment, by way of example only, FIG. 2 depicts a block diagram of the mask defect analysis system 1 of the present invention. First, known and accepted industry techniques are used to manufacture 10 a mask. Next, the mask is inspected 20 using a known inspection tool, such as an optical inspection device (not shown). Note that is it possible to practice the present invention in such a way that the classification of the type of defect (whether clear or opaque) is performed manually by a human operator or by a defect classification tool. Results from the inspection are provided in a mask inspection report 25 (also depicted in FIG. 4). These results can be in tabular form and include the location, size and type (clear or opaque) of any defects identified as being present on the mask. Of course, the inspection report data can also be graphical in the form of intensity contour plots. In another aspect of the present invention, the inspection defect data comprises intensity contour plots from a commercially available inspection tool, such as AIMS. The intensity contour plots (also known as aerial images) contain the size, location and type of defect information similar to that provided by an optical inspection tool. In addition, the intensity contour plots provide information on how or if the defect will be resolved on the wafer when the mask image is transferred to the wafer.

Data from the mask inspection report 25 are then stored in a form readable by a computer program 200 (also discussed below along with FIG. 4).

The following depicts exemplary results from the mask inspection report 25 that are stored in tabular form. Defect Ref X Ref Y Auto Size X Size Y Size User No. loc. (mm) loc. (mm) Type Type Svrty (mm) (mm) Type 2 83.6116 −101.2827 Dim Chrome A Pass 0.500 0.500 3C 3 40.5808 −98.9018 Dim Chrome A Pass 0.500 0.500 2C 4 40.5784 −98.8708 Contam On Chrome D Fail 5.000 3.000 3C 5 89.9094 −95.4073 Dim Chrome A Pass 0.500 0.500 3C 6 63.5390 −93.8937 Contam On Edge A Fail 0.500 0.500 2A 7 82.2504 −93.4359 Dim Chrome A Pass 0.500 1.000 3C 8 76.8741 −90.3492 Dim Chrome A Pass 0.500 1.000 3C 9 79.8490 −89.6193 Dim Chrome A Pass 0.500 0.500 3C 10 30.9956 −88.8151 Dim Chrome A Pass 1.000 1.000 3C 11 39.9058 −83.5845 Dim Chrome A Pass 1.000 1.000 3C 12 40.2300 −82.1064 Contam On Chrome C Warn 1.000 3.000 2C 13 31.8315 −80.8188 Bright Chrome B Pass 0.500 2.000 1A 14 82.6267 −78.7788 Contam On Chrome C Warn 3.000 3.000 2C 15 82.4353 −78.6923 Contam On Chrome A Pass 0.500 1.000 2C 16 82.4026 −78.5518 Dim Chrome A Pass 0.500 1.000 3C 17 10.5894 −72.4460 Dim Chrome A Pass 0.500 0.500 3C 18 41.1788 −71.2059 Contam On Chrome B Pass 1.000 1.500 3C 19 44.1204 −69.1854 Dim Chrome A Pass 0.500 1.000 3C 20 34.9878 −67.6938 Dim Chrome A Pass 1.000 0.500 3C 21 12.2929 −67.6118 Dim Chrome A Pass 1.000 0.500 3C 22 44.9030 −63.5399 Dim Chrome B Pass 1.000 1.500 3C 23 22.5109 −61.3091 Contam On Chrome A Pass 1.000 1.000 1A 24 43.0525 −60.5868 Dim Chrome A Pass 0.500 0.500 3C 25 78.6846 −59.5940 Dim Chrome B Pass 0.500 1.500 3C 26 38.4842 −59.1307 Dim Chrome A Pass 0.500 0.500 3C 27 29.8313 −57.3956 Contam On Edge A Fail 0.500 0.500 4C 28 29.8172 −57.3746 Contam On Edge A Fail 0.500 0.500 4C 29 78.9023 −57.0952 Dim Chrome A Pass 1.000 0.500 3C 30 43.3913 −56.8387 Dim Chrome A Pass 0.500 1.000 3C 31 75.9490 −55.9790 Dim Chrome A Pass 1.000 1.000 3C 32 100.8808 −52.9098 Dim Chrome A Pass 0.500 0.500 3C

As shown in the table, each defect is numbered (1st column) and its planar location is recorded (2nd and 3rd columns). The planar location is determined with respect to an arbitrary position on the mask as chosen by the human operator when the mask is loaded into the inspection tool. Each defect is also categorized as to defect type (4th column), size type (5th column) and severity of defect (6th column). The defect type is determined automatically by the inspection tool and is descriptive of the characteristics of a given defect. Defect size types are grouped into “buckets” and labeled as A, B, C, etc. Severity of defects are automatically classified as “pass” or “fail” by the inspection tool based on the defect type and size type (5th and 6th columns). The size of each defect is also recorded (7th and 8th columns). Finally, a designation of user type or defect type is included (9th column) in which the defect type is determined by a manual microscope review by a human operator and is based on user-specified criteria such as “opaque defect on a line edge” or “isolated clear defect.”

Continuing with FIG. 2, the system generates and adds shapes representing defects 30 corresponding to the results from the inspection defect data. Also, design data 45 (also depicted in FIG. 4) corresponding to the mask level being inspected are retrieved from a design data repository 40, which is essentially a computer database program for storage of large data files. An analysis 50 is performed using the generated shapes 30 and design data 45 in conjunction with a predetermined rule set 60. This analysis step is discussed in more detail in conjunction with FIG. 4. The outcome of the analysis step 50 is to determine if the defect is critical, that is whether the mask should be scrapped 70, repaired 80 or accepted for shipping 90. By applying the above-described system to each defect identified by the inspection tool, an automated system for examining and analyzing defects in the mask is created and can ultimately allow a determination of which defects will cause product failure.

To better illustrate the need for the analysis step, FIGS. 3 a and 3 b depict the effect of a defect on a mask. FIG. 3 a exemplifies the design layout data 45 for a given mask as retrieved from the design data repository 40. This represents the ideal mask layout (i.e., without defects). By comparison, FIG. 3 b depicts shapes 30 generated by the computer program 200 based on the results from the inspection process. A defect is considered to be present on the mask whenever a generated shape 30 is not found in the design layout data 45. However, not all defects are considered harmful to the mask, and certain defects can be ignored if located in unimportant areas of the mask. To illustrate this, in FIG. 3 b it can be seen there is one harmless defect 32 and one fatal defect 34. The defect 32 is considered harmless because it is located in a non-critical area of the mask. However, the fatal defect 34 is so designated because it is in a critical location of the mask and is likely to cause a short between the two adjoining chromium strips. In FIG. 4 the computer program 200 is depicted in block diagram form. As a first step, the program receives input data (e.g., tabular or intensity contour plots) from the mask inspection report 25, which includes the size, location and type (clear or opaque) of any defects located on the mask. Next, the program loads the design layout data 45 such as that depicted in FIG. 3 a. Representative shapes 30, such as those depicted in FIG. 3 b, are then generated by the program for each design level corresponding to the mask being analyzed. At this point, the analysis step 50 from FIG. 2 can be performed using a predetermined rule set 60. This analysis step 50 is expanded in FIG. 4 and includes elements 51 through 59. For instance, the program reads a rule 51 from the rule set 60 that applies to the given mask. Then, using an industry standard design rule checking program, each rule of the rule set 60 is applied 51 to the representative defect shapes 30 to determine whether to repair, accept or scrap the mask based on the current defect. The outcome 53 of a given rule is a designation of “pass” or “fail.” If the defect is a “pass,” the next rule is read and applied 51 until the last rule is reached 57 and a pass report is generated 59. However, if the defect is a “fail,” a failure report 55 is generated. In that event, the mask can either be sent for repair (step 80 from FIG. 2) or scrapped (step 70 from FIG. 2). This analysis is continued and the results of this analysis are tabulated (not shown) until all defects have been analyzed and/or until a predetermined scrap threshold has been reached. As described above, in conjunction with FIG. 2, the results of this analysis ultimately are used to determine if a given mask should be scrapped 70, repaired 80 or accepted for shipment 90.

An exemplary rule set 60 is shown below, in which the following definitions are used:

MINLINE—design rule minimum feature size on the level in question;

MAXLINE—design rule maximum feature size on the level in question;

MINSPACE—design rule minimum space between shapes on levels in question;

VARSPACE—design rule minimum space on the level in question when the space is dependent on the size of the feature;

MASKINSPECT “mask magnification*minimum mask feature inspection limit;

OPPOSITE—shape on complement implant mask; and

BLOB—mask defect (clear or opaque). DT level BLOB width <= MAXLINE on both axes (trench fill) BLOB width >= MINLINE (eliminate possible PLY problems) BLOB to DT >= MINSPACE BLOB to adjacent DTFILL >= MINSPACE (resist adhesion) BLOB to RX >= MINSPACE BLOB to PC >= MINSPACE BLOB to MC >= MINSPACE BLOB to CA >= MINSPACE BLOB to BLOB >= MINSPACE RX level BLOB width >= MINLINE BLOB to DT >= MINSPACE BLOB to RX >= MINSPACE BLOB to adjacent RXFILL >= MINSPACE BLOB to PC >= MINSPACE BLOB to MC >= MINSPACE BLOB to ESDUMMY >= MINSPACE BLOB to CA >= MINSPACE BLOB to BLOB >= MINSPACE PC level BLOB width >= MINLINE (resist adhesion) BLOB to DT >= MINSPACE BLOB to RX >= MINSPACE BLOB to PC >= MINSPACE BLOB to adjacent PCFILL >= MINSPACE BLOB to MC >= MINSPACE BLOB to CA >= MINSPACE BLOB to BLOB >= MINSPACE MC level BLOB width >= MINLINE BLOB to DT >= MINSPACE BLOB to RX >= MINSPACE BLOB to PC >= MINSPACE BLOB to MC >= MINSPACE BLOB to CA >= MINSPACE BLOB to BLOB >= MINSPACE CA level BLOB width >= MINLINE BLOB to DT >= MINSPACE BLOB to RX >= MINSPACE BLOB to PC >= MINSPACE BLOB to MC >= MINSPACE BLOB to CA >= MINSPACE BLOB to M1 >= MINSPACE BLOB to BLOB >= MINSPACE BLOB to CA (same net when BLOB is an extension) >= MASKINSPECT M1 level BLOB width >= MINLINE BLOB width <= MAXLINE (Cu technologies) BLOB to MC >= MINSPACE BLOB to CA >= MINSPACE BLOB to M1 >= VARSPACE BLOB to adjacent M1FILL >= VARSPACE BLOB to V1 >= MINSPACE BLOB to BLOB >= MINSPACE V1 level BLOB width >= MINLINE BLOB width <= MAXLINE (via fill) BLOB to CA >= MINSPACE BLOB to M1 >= MINSPACE BLOB to V1 >= MINSPACE BLOB to M2 >= MINSPACE BLOB to BLOB >= MINSPACE BLOB to V1 (same net when BLOB is an extension) >= MASKINSPECT Mx level BLOB width >= MINLINE BLOB width <= MAXLINE (Cu technologies) BLOB to Vx − 1 >= MINSPACE BLOB to Mx >= VARSPACE BLOB to adjacent Mx >= VARSPACE BLOB to Vx >= MINSPACE BLOB to BLOB >= MINSPACE Vx level BLOB width >= MINLINE BLOB width <= MAXLINE (via fill) BLOB to Mx >= MINSPACE BLOB to Vx − 1 >= MINSPACE BLOB to Vx >= MINSPACE BLOB to Vx + 1 >= MINSPACE BLOB to Mx + 1 >= MINSPACE BLOB to BLOB >= MINSPACE BLOB to Vx (same net when BLOB is an extension) >= MASKINSPECT Implant level (XX) BLOB width >= MINLINE BLOB to OPPOSITE >= MINSPACE BLOB to adjacent RX >= MINSPACE BLOB to adjacent XX >= MINSPACE BLOB to BLOB >= MINSPACE

In the above rule set 60, the identifiers DT, RX, PC, MC, CA, M1, V1, Mx, Vx, and XX refer to design levels that, in turn, make up the mask layers and to which a representative defect shape 30 may be added. These rules essentially specify the acceptable distances, widths, etc. for the defect itself and its relationship to shapes on the same or other design levels.

In an additional embodiment of the present invention, as depicted in the bottom portion of FIG. 2, the inspection and analysis process can be repeated for each mask that passes beyond the inspection process, that is, each mask that has been cleared for shipment 90 or has not been otherwise scrapped 70. An additional inspection is performed 100 on any mask layer ready to be shipped 90, and the results of that inspection are similar to those described above. Design layout data 45 for each mask layer being inspected are again retrieved from the design data repository 40. Thereafter, the computer program 200 generates shapes 110 corresponding to the defect layout data 45 from the inspection tool 100. Then another analysis 120 is performed to determine if the mask 5 should ultimately be rejected 140 or accepted 150.

In another preferred embodiment, by way of example only, FIG. 5 depicts a block diagram for a component defect analysis system, in which different acceptance rules are applied to the defects depending on the criticality.

Conventional mask acceptance criteria allow certain defects located in non-critical portion of a mask to be ignored when determining the disposition of a mask. This means, for example, the mask acceptance criteria for a polysilicon level mask can be manipulated to ignore defects located in certain portions. However, polysilicon wires are not distinguishable from polysilicon gates. Thus, when the mask acceptance criteria for gates are applied to wires during the mask inspection, this may cause the mask to fail certain criteria (e.g., critical dimension control) which are only critical to the gate but not to the wires. This may unnecessarily initiate a critical dimension measurement process which is time consuming, thereby increasing inspection time.

To solve this problem, in FIG. 5, there is shown a process flow chart for determining a final disposition of a component (e.g., mask) by applying different acceptance rules depending on defect criticality. The defects could be opaque, clear or phase variations.

A mask (e.g., mask for polysilicon layer) is designed and produced during a step 200. Simultaneously with the step 200 or independently during a step 230, the mask design data is analyzed preferably by a computer system, to determine critical portions and non-critical portions for corresponding mask acceptance criteria. For example, the mask design data is analyzed to distinguish gates from wires on the polysilicon level, and, as the analysis result, the wires are determined to be the non-critical portions while the gates are determined to be the critical portions. The analysis result is stored to a file, preferably a computer readable data file, which includes locations and sizes of gates.

Subsequently, the mask is inspected for defects by using an inspection tool during an inspect step 210. If no defect is located, the masked is routed to a shipping step 260. If defects are located, another file is created from the inspection step, which stores the locations and sizes of defects identified by the inspection tool. In a step 220, the two files are analyzed together to determine if defects are located in the critical portions or the non-critical portions of the mask.

Based on the analysis, the defects are sorted into several classifications. For example, the defects located in the critical portions are classified as critical defects and the defects located outside of the critical portions are classified as non-critical defects. Different acceptance rules are applied to the defects depending on the defect classification, and the final disposition of the mask is determined based on the mask's defect classifications. A standard acceptance rule is applied to the defects located in the critical portions of the mask while a loose acceptance rule is applied to the defects located outside of the critical portions. When the loose acceptance rule is applied, the non-critical defects are considered as the candidates for a looser mask acceptance criteria. For example, as long as the minimum design rules are not violated, a mask having a polysilicon wire having width or transmissivity larger than that of the standard polysilicon gate can be accepted and shipped as shown in a step 260. The critical dimension measurement is selectively performed only to the critical defects and routed to a repair step 240 or a scrapping step 250. The repaired masks are routed to the inspection step 210 to repeat the entire mask disposition process.

The spatial component of the looser acceptance rules could be defined as a set of rules used to identify regions of the layout which in turn could be used when re-inspecting the repaired mask. This procedure results in fewer scrapped masks due to repair failures. Also, the entire processing steps can be implemented into a computer software program which can control the mask inspection tool.

Thus, according to the present invention, features in the layout could be sorted into critical or non-critical portions. Time consuming critical dimension measurements are performed restrictedly to the critical portions, thereby speeding up the measurement process. Feedback from this mask disposition process could also be incorporated for macros which can be used on other masks.

While the invention has been described in terms of preferred embodiments, and specific embodiments by way of example in the drawings are described in detail, it should be understood that the drawings and detailed description thereto are not intended to limit the invention to the particular form disclosed. To the contrary, those skilled in the art will recognize that the present invention can be practiced with modifications, equivalents and alternatives within the spirit and scope of the appended claims.

Having thus described our invention, what we claim as new and desire to secure by Letters Patent is as follows. 

1. A method for evaluating the effect of defects on components in a semiconductor manufacturing process, said method comprising the steps of: identifying critical portions of a component; inspecting the component for defects; analyzing locations of the defects to classify said defects into critical defects and non-critical defects; and determining a final disposition of the component by applying different acceptance rules to the critical defects and the non-critical defects.
 2. The method of claim 1, wherein the defects located within the critical portions are classified as the critical defects, and the defects located outside of the critical portions are classified as the non-critical defects.
 3. The method of claim 2, wherein the acceptance rules comprises a standard acceptance rule applied to said critical defect and a loose acceptance rule applied to said non-critical defects.
 4. The method of claim 3, wherein said final disposition of the component is selected from accepting, repairing or scrapping the component.
 5. The method of claim 4, wherein the component is a mask used for a semiconductor manufacturing process.
 6. The system for evaluating the effect of defects in components in a semiconductor manufacturing process, said system comprising: an inspection tool for locating defects in a component; and a computer system for classifying said defects into critical defects and non-critical defects based on locations of said defects and critical portions of said component, wherein the computer systems determines a final disposition of the component by applying different acceptance rules to the critical defects and the non-critical defects.
 7. The system of claim 6, wherein said computer system classifies the defects located within said critical portions as the critical defects and the defects located outside of said critical portions as the non-critical defects.
 8. The system of claim 7, the acceptance rules comprising a standard acceptance rule and a loose acceptance rule, wherein the computer system applies the standard acceptance rule to said critical defects and the loose acceptance rule to said non-critical defects.
 9. The system of claim 8, wherein the said final disposition of the component is selected from accepting, repairing or scrapping the component.
 10. The method of claim 9, wherein the component is a mask used for a semiconductor manufacturing process.
 11. A computer readable medium comprising codes for causing a computer to implement steps of a method for evaluating the effect of defects in components, the method comprising the steps of: identifying critical portions of a component; inspecting the component for defects; analyzing locations of the defects to classify said defects into critical defects and non-critical defects; and determining a final disposition of the component by applying different acceptance rules to the critical defects and the non-critical defects.
 12. The method of claim 11, wherein the defects located within the critical portions are classified as the critical defects, and the defects located outside of the critical portions are classified as the non-critical defects.
 13. The method of claim 12, the acceptance rules comprising a standard acceptance rule and a loose acceptance rule, wherein the standard acceptance rule is applied to said critical defects and the loose acceptance rule is applied to said non-critical defects.
 14. The method of claim 13, wherein said final disposition of the component is selected from accepting, repairing or scrapping the component.
 15. The method of claim 14, wherein the component is a mask used for a semiconductor manufacturing process.
 16. A method of evaluating the effect of defects on components in a semiconductor manufacturing process, said method comprising: inspecting a component for defects using an inspection tool; generating shapes representing the defects; performing an analysis using the design data, the generated shapes, and a pre-determined rule set to determine whether the defects are critical defects and non-critical defects, applying different acceptance rules to the critical defects and the non-critical defects to provide a final disposition of the component.
 17. The method of claim 16, wherein the applying different acceptance rules comprises: applying a first acceptance rule to the defects located in critical portions of the component; and applying a second acceptance rule, that is looser than the first acceptance rule, to the defects located outside the critical portions of the component.
 18. The method of claim 16, further comprising: storing defect inspection data from the inspection tool; retrieving design data from a design data repository corresponding to the component being inspected; reading a first rule from a predetermined rule set of a plurality of rules; and determining whether to repair, accept, or scrap the component based upon the defect by applying the first rule to the generated shape.
 19. The method of claim 18, wherein the first rule one of: specifies the minimum acceptable distance between the defect and an other shape on a same design level of a mask; and specifies the minimum acceptable distance between the defect and an other shape on a different design level of a mask.
 20. The method of claim 18, further comprising: reading a second rule from the predetermined rule set of a plurality of rules; and determining whether to repair, accept, or scrap the component based upon the defect by applying the second rule to the generated shape. 